View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 23839U 26121.23378235 +.00000000 +00000-0 +00000-0 0 00003
2 23839 10.5060 47.0605 0003834 339.3792 230.2651 0.99993379 02
| Epoch (UTC): | 01 May 2026 05:36:38 |
| Eccentricity: | 0.0003834 |
| inclination: | 10.5060° |
| perigee height: | 35849 km |
| apogee height: | 35881 km |
| right ascension of ascending node: | 47.0605° |
| argument of perigee: | 339.3792° |
| revolutions per day: | 0.99993379 |
| mean anomaly at epoch: | 230.2651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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